Mach Angle
theta_m = asin(1/M_a)
What it says
The half-angle of the shock cone trailing a supersonic body.
Symbols
| Symbol | Quantity | Dimension |
|---|---|---|
theta_m | Mach angle (rad) | 1 |
M_a | Mach number (dimensionless) | 1 |
Work it out
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Fill in all but one: M_a, theta_m are all empty.
Filed under Fluid dynamics · derive through it in the explorer